C64200 Aluminum Bronze: Machining Parameters and Wear Properties

When a design demands tensile strength above 550 MPa, seawater corrosion resistance, and the ability to handle sliding wear without galling, engineers often reach for aluminum bronze — and C64200 is the most widely available wrought grade in that family. It combines roughly 7% aluminum with 3% iron in a copper matrix, delivering a hardness envelope (Brinell 170–210) comparable to some quenched-and-tempered alloy steels. But that same hardness is what makes it a challenge on the CNC floor: C64200 machines differently from both brass and stainless steel, and treating it like either will cost you tool life. This article covers what C64200 is, how it behaves under the tool, and what belongs on your drawing before quoting a job.

Where C64200 Sits in the Aluminum Bronze Family

C64200 is a nickel-free wrought aluminum bronze, designated CuAl8Fe3 under the European system and covered by ASTM B150/B150M for rod, bar, and shapes. Unlike nickel-aluminum bronzes (C63000 with ~5% Ni, or cast C95500), C64200 relies on iron-rich precipitates for grain refinement and elevated-temperature strength rather than nickel intermetallics.

The absence of deliberate nickel keeps cost moderate relative to C63000 while retaining enough corrosion resistance for marine hardware, pump shafts, and valve stems where seawater or brackish water is the working medium. Designers sometimes call C64200 a “budget aluminum bronze” — that’s directionally correct, but the trade-off is lower toughness at sub-zero temperatures and slightly reduced cavitation resistance compared to nickel-bearing grades.

Chemical Composition per ASTM B150

The composition below is per ASTM B150/B150M for UNS C64200 wrought products. Values are weight-percent maxima unless a range is given.

Element Content (wt%) Role in the Alloy
Aluminum (Al) 6.0 – 8.0 Primary strengthener; provides seawater corrosion resistance
Iron (Fe) 2.0 – 4.0 Grain refiner via Fe-rich precipitates; improves high-temperature strength
Nickel (Ni) ≤ 0.25 Tramp element — kept low to distinguish from Ni-Al-bronze grades
Manganese (Mn) ≤ 0.10 Deoxidizer; kept low
Silicon (Si) ≤ 0.50 Residual
Tin (Sn) ≤ 0.20 Residual
Zinc (Zn) ≤ 0.50 Residual; higher levels degrade hot workability
Copper (Cu) Remainder Matrix (~89% nominal)

Reputable mills often hold an internal spec of 6.5–7.5% Al — above 8% pushes the material toward beta-rich embrittlement. The total of other named elements is typically under 1%, so the alloy’s behavior is overwhelmingly driven by aluminum and iron content.

Mechanical Properties by Temper

ASTM B150 defines minimum tensile properties for annealed (O61) and as-extruded/hot-finished conditions. Commercial bar stock routinely exceeds these minima by 10–20%.

Property Annealed (O61) As-Extruded / Hot-Finished Test Standard
Tensile Strength ≥ 485 MPa (70 ksi) ≥ 550 MPa (80 ksi) ASTM E8 / ISO 6892-1
Yield Strength (0.2%) ≥ 240 MPa (35 ksi) ≥ 275 MPa (40 ksi) ASTM E8
Elongation in 4D ≥ 22% ≥ 15% ASTM E8
Brinell Hardness 140–180 HBW 170–210 HBW ASTM E10 / ISO 6506-1
Modulus of Elasticity ~115 GPa (17,000 ksi) at RT Resonant frequency method
Density ~7.7 g/cm³

Important: Aluminum bronze does not respond to martensitic heat treatment. The strength difference between O61 and hot-finished conditions comes from retained hot-work substructure, not phase transformation. If your drawing calls for “hardened” C64200, clarify whether you mean as-extruded or a specific hardness range — C64200 cannot exceed ~210 HBW without cold working, and that’s only available in thin sections or drawn wire.

Corrosion and Wear Behavior

In seawater (natural or synthetic per ASTM D1141), C64200 forms a protective alumina-rich passive film yielding corrosion rates under 0.025 mm/yr in quiet immersion at 20°C. Under flowing conditions (3–5 m/s), the film remains adherent and self-healing — a key advantage over brass and carbon steel. In stagnant or sulfide-polluted seawater, selective dealumification is a risk, but C64200 with iron above 3% shows measurably better resistance than low-iron aluminum bronze grades.

For wear: the 170–210 HBW hardness plus the low-friction oxide film gives C64200 good galling resistance against stainless steel counterfaces. In unlubricated pin-on-disc testing (10 N load, ASTM G99 geometry), C64200 typically shows wear rates under 5 × 10⁻⁵ mm³/N·m against 316 stainless steel — competitive with phosphor bronze and clearly better than naval brass (C46400). However, C64200 is not a bearing bronze: it lacks lead or graphite pockets needed for marginal-lubrication conditions. Use it for guides, gibs, and wear plates where full-film or boundary lubrication is maintained.

CNC Machining Characteristics

C64200 machines like a short-chipping alloy — more like medium-carbon steel than brass. Chips break into small, hard segments rather than long stringy ribbons typical of 316 stainless. That’s good for chip evacuation in deep holes, but the abrasive aluminum-iron intermetallics accelerate flank wear on carbide tools.

  • Chip form: Short, segmented Type-C chips above 80 m/min. Below 50 m/min, chips may become powdery and abrasive.
  • Work hardening: Mild to moderate. Unlike austenitic stainless, C64200 does not work-harden rapidly. The lower elastic modulus (115 GPa vs ~200 GPa for steel) makes tool deflection — not work hardening — the bigger accuracy risk on slender parts.
  • Built-up edge: Low with sharp carbide and adequate cooling. HSS tools at high speeds can cause aluminum transfer, producing a false edge that degrades finish.
  • Thermal conductivity: ~50 W/m·K — higher than stainless (~16) but lower than free-cutting brass (~120). Heat concentrates at the tool tip; flood coolant is recommended for continuous cuts.

Starting-Point Cutting Parameters

These are suggested starting points for C64200 bar stock (as-extruded, ~190 HBW) on a rigid CNC lathe or VMC with coated carbide. They are not production guarantees — machine rigidity, toolholder overhang, coolant pressure, and part geometry will shift these numbers.

Operation Speed Feed Depth of Cut Tool Grade / Coating
Turning (rough) 90–150 m/min (300–500 SFM) 0.15–0.30 mm/rev 1.5–4.0 mm CVD TiCN/Al₂O₃ carbide, K10–K20
Turning (finish) 120–180 m/min (400–600 SFM) 0.05–0.12 mm/rev 0.3–0.8 mm PVD TiAlN carbide, positive rake 8°–12°
Milling (shoulder) 70–120 m/min (230–400 SFM) 0.08–0.18 mm/tooth 0.5–2.5 mm radial TiAlN solid carbide, 4-flute, helix 35°–45°
Drilling (ø 6–12 mm) 40–70 m/min (130–230 SFM) 0.08–0.20 mm/rev TiAlN carbide, split point 140°
Threading (single-point) 15–30 m/min (50–100 SFM) Pitch-dependent 0.05–0.15 mm/pass PVD TiN carbide, full-profile insert

Coolant: Semi-synthetic at 8–12%, ≥10 bar through-tool or well-directed flood. MQL is possible for light finishing but not recommended for drilling. With these parameters, a TiAlN insert in continuous turning should reach 25–40 minutes before flank wear exceeds VB 0.3 mm. For interrupted cuts (milling, grooving), reduce speed by 15–20%.

Surface Finishing

C64200 accepts standard post-processing:

  • As-machined: Ra 0.8–1.6 μm achievable with sharp finishing insert and steady setup. Inspect insert edge condition before finish passes — worn tools produce tearing, not burnishing.
  • Electropolishing: Effective for deburring and brightening.
  • Plating: Nickel or chrome for cosmetic or additional wear purposes. Zinc plating offers no benefit on an already corrosion-resistant copper alloy.
  • Welding: GTAW with ERCuAl-A2 filler achieves tensile strength above 480 MPa as-welded. Preheat to 150°C and slow cool to avoid cracking in sections over 12 mm.

Applications

  • Marine pump shafts and impellers: Good seawater resistance without Ni-Al-bronze cost.
  • Valve stems and seats: Holds up under repeated seating cycles in steam and water to ~290°C.
  • Wear plates and slide guides: Low-friction oxide film reduces stick-slip against stainless ways.
  • Fasteners for marine/chemical environments: C64200 bolts per ASTM F468 perform well where stainless fasteners suffer crevice corrosion.
  • Aerospace landing gear bushings: High bearing load capacity without lead content.

Comparison with Related Alloys

Property (as-extruded, typical) C64200 (Al-Bronze) C63000 (Ni-Al-Bronze) C46400 (Naval Brass) C51000 (Phos. Bronze)
Tensile Strength ≥ 550 MPa ≥ 690 MPa ≥ 380 MPa ≥ 340 MPa
Hardness 170–210 HBW 200–240 HBW 90–110 HBW 80–100 HBW
Seawater Corrosion <0.025 mm/yr <0.020 mm/yr 0.025–0.050 mm/yr <0.030 mm/yr
Machinability ~50% ~40% ~70% ~20%
Relative Cost 1.0 1.4–1.6 0.6–0.8 0.7–0.9

C64200 offers a sweet spot: substantially stronger than naval brass, free from the dezincification that limits C46400 in seawater, and less expensive than nickel-bearing C63000. However, “approximately equivalent” is not “interchangeable” — a bushing rated for C63000 at 690 MPa won’t meet that requirement in C64200 without a section increase, and a part designed around phosphor bronze’s conformability may fail in C64200 under boundary lubrication.

What to Include in Your RFQ

To get a meaningful quote for C64200 machined parts, include these on your drawing:

  • Material and temper: UNS C64200 per ASTM B150 (or EN CuAl8Fe3), with temper — O61 (annealed) or hot-finished.
  • Mechanical requirements (if beyond standard): hardness range (e.g., 170–200 HBW) or tensile per ASTM E8.
  • Quantity and preferred stock size: C64200 bar is commonly available from 12 mm to 150 mm diameter.
  • Tolerances: ISO 2768-m or tighter. Specify GD&T for concentricity on shaft features.
  • Surface finish: Ra requirement on bearing surfaces, seal diameters, and threads.
  • Post-processing: Stress relief anneal, electropolish, plating, or NDE (dye penetrant).
  • Inspection: Certificate of conformance, dimensional report, or material certs with heat traceability.

Send your drawing and specifications, and we can evaluate whether C64200 — or perhaps a nickel-aluminum bronze or a different copper alloy — fits your operating conditions, budget, and quantity.

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